Calculation of the laminar viscous shock layer on a blunt biconic body at incidence to supersonic and hypersonic flow
- 24 January 1977
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Hypersonic viscous static stability of a sharp 5-deg cone at incidenceAIAA Journal, 1976
- A Direct Comparison of Analytical and Experimental Surface and Flow-Field Data on a 4-Deg Cone at Incidence in a Hypersonic Stream with Laminar Boundary LayersPublished by Defense Technical Information Center (DTIC) ,1976
- Calculation of the flow on a blunted cone at high angle of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- An Implicit Method for Three-Dimensional Viscous Flow with Application to Cones at Angle of AttackPublished by Defense Technical Information Center (DTIC) ,1973
- Numerical solution of the hypersonic viscous shock-layer equationsAIAA Journal, 1970